DE3863436D1 - RUDDER CONTROL. - Google Patents

RUDDER CONTROL.

Info

Publication number
DE3863436D1
DE3863436D1 DE8888101279T DE3863436T DE3863436D1 DE 3863436 D1 DE3863436 D1 DE 3863436D1 DE 8888101279 T DE8888101279 T DE 8888101279T DE 3863436 T DE3863436 T DE 3863436T DE 3863436 D1 DE3863436 D1 DE 3863436D1
Authority
DE
Germany
Prior art keywords
rudder control
rudder
control
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
DE8888101279T
Other languages
German (de)
Inventor
Des Erfinders Beantragt Teilnichtnennung
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Diehl Verwaltungs Stiftung
Original Assignee
Diehl GmbH and Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Diehl GmbH and Co filed Critical Diehl GmbH and Co
Priority to DE8888101279T priority Critical patent/DE3863436D1/en
Application granted granted Critical
Publication of DE3863436D1 publication Critical patent/DE3863436D1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/34—Transmitting means without power amplification or where power amplification is irrelevant mechanical using toothed gearing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
DE8888101279T 1987-01-30 1988-01-29 RUDDER CONTROL. Expired - Fee Related DE3863436D1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE8888101279T DE3863436D1 (en) 1987-01-30 1988-01-29 RUDDER CONTROL.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19873702733 DE3702733A1 (en) 1987-01-30 1987-01-30 RUDDER CONTROL
DE8888101279T DE3863436D1 (en) 1987-01-30 1988-01-29 RUDDER CONTROL.

Publications (1)

Publication Number Publication Date
DE3863436D1 true DE3863436D1 (en) 1991-08-08

Family

ID=6319839

Family Applications (2)

Application Number Title Priority Date Filing Date
DE19873702733 Granted DE3702733A1 (en) 1987-01-30 1987-01-30 RUDDER CONTROL
DE8888101279T Expired - Fee Related DE3863436D1 (en) 1987-01-30 1988-01-29 RUDDER CONTROL.

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE19873702733 Granted DE3702733A1 (en) 1987-01-30 1987-01-30 RUDDER CONTROL

Country Status (3)

Country Link
US (1) US5040745A (en)
EP (1) EP0276867B1 (en)
DE (2) DE3702733A1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3837481C2 (en) * 1988-11-04 1995-05-18 Deutsche Aerospace Gear for pivoting a mirror
DE4009549A1 (en) * 1990-03-24 1991-09-26 Messerschmitt Boelkow Blohm Rudder drive with electromotor driving threaded shaft - accepting lead-nut coupled to forked lever
DE4019482A1 (en) * 1990-06-19 1992-01-09 Diehl Gmbh & Co RUDDER CONTROL
DE4135557C2 (en) * 1991-10-29 1999-05-06 Diehl Stiftung & Co Rudder control device
DE4438010A1 (en) * 1994-10-25 1996-05-02 Diehl Gmbh & Co Target-seeking missile with rotation about its longitudinal axis
DE19617221C2 (en) * 1996-04-30 1999-07-01 Diehl Stiftung & Co Steerable projectile that can be used as a mortar
US5950963A (en) * 1997-10-09 1999-09-14 Versatron Corporation Fin lock mechanism
DE19922693A1 (en) * 1999-05-18 2000-11-23 Diehl Stiftung & Co Control device for the rudder of a missile
RU2503919C1 (en) * 2012-10-09 2014-01-10 Открытое акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Drive of carrying control plane of airborne vehicle
DE102015005135A1 (en) * 2015-04-22 2016-10-27 Diehl Bgt Defence Gmbh & Co. Kg Missile rudder system
CN111207630B (en) * 2020-01-10 2021-03-19 蓝箭航天空间科技股份有限公司 Rocket flight attitude control method

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE745795C (en) * 1938-08-31 1944-12-01 Auxiliary rudder drive for aircraft
FR857515A (en) * 1938-09-14 1940-09-17 Dornier Werke Gmbh Motor driven rudder
DE746809C (en) * 1941-06-12 1944-08-25 Hans Belart Dipl Ing Tail unit on aircraft
US2504767A (en) * 1946-03-28 1950-04-18 Vickers Armstrongs Ltd Aircraft with adjustable wings
US3305194A (en) * 1960-03-08 1967-02-21 Robert G Conard Wind-insensitive missile
US3200587A (en) * 1961-09-15 1965-08-17 Gen Motors Corp Rocket vehicle attitude control
FR1424606A (en) * 1964-12-23 1966-01-14 Hamburger Flugzeugbau Gmbh Device for adjusting the angle of attack, in particular for aircraft
US3568957A (en) * 1968-11-13 1971-03-09 Mc Donnell Douglas Corp Long structural column support
US4052024A (en) * 1976-05-12 1977-10-04 The United States Of America As Represented By The Secretary Of The Army Pneumatic gear motor application
US4180222A (en) * 1976-12-27 1979-12-25 Lockheed Aircraft Corporation Aileron segment control for a flaperon system
DE3441533A1 (en) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg COUPLING DEVICE BETWEEN A LINEAR ACTUATOR AND A SWIVELING ELEMENT, IN PARTICULAR A CONTROL LEVER
DE3442899C1 (en) * 1984-11-24 1986-06-12 Dornier System Gmbh, 7990 Friedrichshafen Rudder drive

Also Published As

Publication number Publication date
EP0276867B1 (en) 1991-07-03
DE3702733A1 (en) 1988-08-11
EP0276867A3 (en) 1989-07-26
US5040745A (en) 1991-08-20
DE3702733C2 (en) 1989-05-24
EP0276867A2 (en) 1988-08-03

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee